Electromechanical Resonant Ice Protection Systems: Analysis of Fracture Propagation Mechanisms

Author:

Budinger Marc1,Pommier-Budinger Valérie2,Bennani Lokman3,Rouset Pierrick1,Bonaccurso Elmar4,Dezitter Fabien5

Affiliation:

1. Clément Ader Institute, Université de Toulouse, CNRS-INSA-ISAE-Mines Albi-UPS, Toulouse 31400, France

2. National Higher French Institute of Aeronautics and Space (ISAE SUPAERO), Université de Toulouse, Toulouse 31400, France

3. ONERA, Toulouse 31055, France

4. AIRBUS Central R&T, Munich 82024, Germany

5. Airbus Helicopters, Marignane 13700, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference31 articles.

1. SeppingsR. A. “Investigation of Ice Removal from Cooled Metal Surfaces,” Ph.D. Dissertation, Imperial College London, Univ. of London, London, 2006.

2. Mechatronic Development of Self-Actuating In-Flight Deicing Structures

3. Piezoelectric Transducer Actuated Leading Edge De-Icing with Simultaneous Shear and Impulse Forces

4. PalaciosJ. L. “Design, Fabrication, and Testing of an Ultrasonic De-Icing System for Helicopter Rotor Blades,” Ph.D. Thesis, Pennsylvania State Univ., State College, 2008.

5. Instantaneous De-Icing of Freezer Ice via Ultrasonic Actuation

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